Raytheon 1900D
Service difficulty reports · 7,152
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900D' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '1900D' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA020510017Window · failed(CAN) ON CLIMB OUT THROUGH APPROXIMATELY 17,000 FT EXPERIENCED A LOUD BANG IN THE CABIN. REALIZING CABIN WAS DECOMPRESSED, THE CREW REQUESTED IMMEDIATE DESCENT. THE CREW DECIDED NOT TO DEPLOY PASSENGER MASKS SINCE THEY WERE AT A LOW ALTITUDE AND WOULD CAUSE MOSDR NSVA0210Wheel · separatedAIR DISPATCH RECEIVED A REPORT THAT AIRCRAFT HAD LOST THE NR 4 MAIN WHEEL ASSEMBLY DURING TAKEOFF. CREW CONTINUED TO IAD WHERE THE TOWER CONFIRMED THAT A WHEEL WAS MISSING. CREW DECLARED AN IN FLIGHT EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTEDSDR CA020424001Gyro · malfunctioned(CAN) ON DEPARTURE GOT YELLOW HEADING FLAG, WHICH WAS CLEARED, HAPPENED AGAIN AT TOC, CLEARED. IN CRUISE GOT RED HEADING ON NR 1 SYSTEM, SWITCHED TO HDG ALL ON NR 2 REVERSION PANEL. RETURNED TO YYC. MAINTENANCE REPLACED THE NR 1 DIRECTIONAL GYRO, TESTEDSDR GLBA2002055Flow Divider · leakingFUEL ODOR IN COCKPIT ON TAXI, INSPECTED FOUND RIGHT FUEL FLOW DIVIDER LEAKING, REPLACED OPS CHECKED SYSTEM SATISFACTORYSDR S2YA02015Engine · making metalFLT 1270 - MKE-CMH - THE LEFT OIL PRESSURE ILLUMINATED IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING. OUT STATION MAINTENANCE SERVICED THE LEFT ENGINE WITH OIL AND THE CREW DID A GROUND RUN. AFTER SHUTDOWN OF THE GROUND RUN, THERE WAS FLAMES COMING OUT OF SDR CA020417001Windshield · cracked(CAN) DURING CLIMBOUT FROM YYC THE CO PLIOTS WINDSHIELD CRACKED. AIRCRAFT WAS LEVELED OFF AND RETURNED TO AIRPORT. THE OUTER PLY OF WINDSHIELD WAS CRACKED WITH NO APPARENT REASON SUCH AS IMPACT. THE WINDSHIELD WAS REPLACED AND THE OLD SENT FOR INVESTIGATION.SDR GLBA2002052Tach Generator · intermittentLEFT N1 FLUXUATION, REPLACED TAC GEN OPS CHECKED SATISFACTORYSDR GUU2002F00003Computer · malfunctionedDURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.SDR GLBA2002051Altimeter · failedCAPTAINS ALTIMETER FLAGGED. REPLACED, OPS CHECKED SATISFACTORY.SDR GLBA2002050Altimeter · inoperativeNR 1 ALTIMETER FAILED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.SDR GUU2002F00001Bolt · looseAT SCHEDULED ROUTINE INSPECTION VERTICAL FIN LOWER ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.SDR CA020422004Keel · worn(CAN) DURING INVESTIGATION OF A DC LOAD SHARE PROBLEM BETWEEN BOTH GENERATOR FOUND FOUR WIRES CHAFFED IN THE LT NACELLE ON THE OUTBOARD KEEL WEB ASSY. THE DAMMAGE ON THE KEEL WEB WAS DUE TO ELECTRICAL ARCING BETWEEN THE WIRE AND THE KEEL WEB ASSY. NO PROTECTIOSDR GLBA2002048Sensor · failedLEFT & RIGHT ENVIRONMENTAL FAILURE. REPLACED TEMP SENSOR.SDR GLBA2002049Converter · failedRIGHT WINDSHIELD WIPER FAILED. REPLACED CONVERTER, OPS CHECKED SATISFACTORY.SDR CA020515014Rivet · sheared(CAN) UPON INVESTIGATION OF A FUEL LEAK LT AUXILIARY FUEL TANK, "PRC" REMOVED AND FOUND 6 RIVET HEADS ATTACHED TO THE "PRC", AT LT KEEL RIB INSTALLATION BL.91.75. SHANK'S REMOVED AND NEW RIVETS INSTALLED.SDR GLBA2002047Altimeter · inaccurateCAPTAINS ALTIMETER INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002046Warning System · malfunctionedRIGHT ENVIRONMENTAL FAIL ILLUMINATED. COULD NOT DUPLICATE FAULT.SDR GLBA2002045Altimeter · inaccurateCAPTAINS ALTIMETER ALTITUDE INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYSDR CA020419003Relay · corroded(CAN) DURING PREFLIGHT CHECK PILOT PULLED THE FIRE HANDLE TO CHECK THE FUEL SHUTOFF VALVE OPERATION, WHEN HE PUSH IT BACK THE VALVE STAYED CLOSED.AFTER INVESTIGATION WE FOUND ALL THE CONTACT ON RELAY (A236K1)CORRODED AND FEW PIN BROKEN. RELAY AND WIRE WAS REPSDR CA020506004Socket · cracked(CAN) DURING A ROUTINE INSPECTION A CRACK WAS NOTED IN THE AREA OF THE MAIN LANDING GEAR LOWER TORQUE KNEE LUGS.THE PISTON AND AXLE ASSY WAS REPLACED.THE CRACKED AXLE AND PISTON ASSY WERE SENT FOR O/H.THE SOCKET ASSY WAS REPLACED AT THE OVERHAUL FACILITY (CRACSDR GLBA2002044Indicator · failedRIGHT ITT INDICATOR FAILED ON CLIMBOUT. REPLACED INDICATOR.SDR 2002FA0000549Keelbeam · crackedSMALL CRACK FOUND ON RIGHT HAND FORWARD OUTBOARD WHEEL WELL KEEL AT UPPER GEAR FENDER SUPPORT ANGLE (SUPPORT ANGLE IS PART OF KEEL CASTING).SDR B2P2002F00002Screw · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKAGE FROM BLADE SOCKETS. PROPELLER WAS DISASSEMBLED AND INSPECTED. UPON FURTHER INVESTIGATION, THE PRELOAD PLATE SCREWS WERE SEVERELY WORN AND ONE WAS BROKEN IN TWO PIECES. LOSDR B2P2002F00001Bearing Race · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSEMBLY IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583 HAD FAILED COMPLETELY AND WERE IN MANY PIECES. POSSIBLE CAUSE COULD BESDR B2P2002F00000Bearing Race · brokenCUSTOMER REMOVED PROPELLER FROM SERVICE DUE TO EXCESSIVE BLADE PLAY AND GREASE LEAKING FROM BLADE SOCKETS. UPON DISASSEMBLY, IT WAS NOTED THAT THE BEARING RACES ON BLADES (SN 2579 AND 2583) HAD FAILED COMPLETELY AND WERE IN MANY PIECES. POSSIBLE CAUSE COULD SDR GLBA2002043Switch · inoperativeLEFT PUSH TO-TALK SWITCH FAILED REPLACED OPS CHECKED SATISFACTORYSDR CA020405003Line · chafed(CAN) THE L/H FUEL CROSS TRANSFER TUBE WAS FOUND CHAFED THROUGH AND SEEPING FUEL. THE WEAR MARK ON THE TUBE MEASURED APPROXIMATELY 5/16 INCH IN LENGTH X 1/8 INCH IN WIDTH. REF: IPC 28-20-00. WEAR OCCURRED FROM THE WIRE BUNDLE COVERING OF THE GEAR UPLOCK MICROSSDR JJB2002F00000Link · dischargedDURING ROUTINE INSPECTION, FOUND LEFT ENGINE ANTI-ICE VANE DOOR SHOCK LINKS MISSING PARTS AND DOOR DISCONNECTED. NOTE: DOWEL PINS FELL OUTOF SPRING RETAINER.SDR CA020419002Relay · corroded(CAN) DURING PREFLIGHT CHECK PILOT PULLED THE LT FIRE HANDLE TO CHECK THE SHUTTOFF VALVE OPERATION, WHEN HE PUSH BACK THE HANDLE THE VALVE STAYED CLOSED. SEVERAL TRIES WERE NECESSARY TO OPEN THE VALVE. DURING TROUBLESHOOTING, THE PROBLEM DID NOT REOCCUR BUT AFSDR GLBA2002039Warning System · malfunctionedOVER FLEW MCK, BATT-TIE ANNUN, OPENED IN FLIGHT, WOULD NOT RESET. PERFORMED SELF TEST SEVERAL TIMES, NO FAULT FOUND. INSPECTED AND CHECKED OKAY FOR SERVICE.SDR GLBA2002037Encoder · inaccurate#2 ENCODER REPORTED HIGH BY ATC, REPLACED ENCODING ALTIMETER OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002038Altimeter · malfunctionedALTIMETER SPLIT. COULD NOT DUPLICATE, OPS CHECKED SATISFACTORY.SDR GLBA2002036Wire · brokenOIL TEMP INDICATOR FAILED. REPAIRED BROKEN WIRE, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2002034Motor · inoperativeLANDING GEAR RELAY C/B POPPED, REPLACED HYDRAULIC MOTOR OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002032Valve · leakingLEFT AND RIGHT ENVIROMENTAL FAILURE AND LOSS OF PRESSURIZATION, REPLACED INSTRUMENT AIR VALVESDR GLBA2002033Torque Link · damagedLEFT MAIN TORQUE KNEE SEPARATED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.SDR GLBA2002035A/C Pack · failedLEFT ENVIRONMENTAL FAILURE ON T/O.SDR GLBA2002031Transmitter · intermittentRT TORQUE INDICATOR FAILED, REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORYSDR CA020307003Bracket · cracked(CAN) CREW BEGAN TAXI FROM OUTSTATION&NOTED THAT "GREEN" NOSEGEAR IND. EXTINGUISHED&"RED" UNSAFE IND. ILLUMINATED. A/C SHUTDOWN, PAX DEPLANED&A/C CHOCKED. MAINT FOUND BRACKET THAT PROVIDES DO WN MICRO SWITCH STRIKE PLATE HAD CRACKED ACROSS ATTACHMENT FLANGE&WOSDR GLBA2002030Switch · out of adjustFLAPS STUCK AT 17 PERCENT, ADJUSTED FLAP SAFTEY SWITCH OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002029Connector · looseLEFT GENERATOR TIE ILLUMINATED ON T/O, RESECURED CONNECTOR PLUG & PCB OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002027Motor · failedFLAPS STUCK AT 17 PERCENT.SDR GLBA2002028Tach Generator · fluctuatesLEFT N1 INDICATOR FLUCTUATING. REPLACED TACH GEN, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2002026Warning System · malfunctionedLEFT GEN TIE ANNUNCIATOR ILLUMINATED IN-FLIGHT. COULD NOT DUPLICATE.SDR CA020227005Actuator · inoperative(CAN) DURING NORMAL APPRAOCH, CREW EXTENDED LANDING GEAR BUT DID NOT GET A NOSE GREEN. GEAR WAS CYCLED WITHOUT CHANGE. EMERGENCY PROCEDURES PROVIDED FOR MANUAL EXTENSION BUT STILL WITHOUT GREEN. DUE TO SYSTEM WIRING, THE GEAR WAS ASSERTAINED DOWN DUE TO THE ABSDR AMW2002F00001Hose · leakingENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCED POWER ON THE LEFT ENGINE AND LANDED WITHOUT INCIDENT.SDR CA020225001Bearing · corroded(CAN) R/H AILERON FOUND WITH EXSCESSIVE UP AND DOWN PLAY.PLAY WAS CAUSED DUE TO R/H AILERON TERMINAL BELLCRANK BEARING WORN.BALL INSIDE BEARING WAS FOUND HEAVILY CORRODED AND OUT OF SHAPE.SDR 2002F00272Door · out of rigDURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTERIOR OF THE AIRCRAFT. AIRCRAFT MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, AND ADJUSTED THE DOOR PER MAINTENANCE INSTRUCTION. RETURNED TO SDR CA020411009Wire · chafed(CAN) AFTER DEPARTURE, CREW NOTICED FAINT ODOUR AND SAW AUTOFEATHER CB WAS POPPED. ELECTED TO RETURN AND DURING DECENT ODOUR INCREASED ACCOMPANIED BY SMOKE. DEPLOYED AND DONNED O2 MASKS. WENT THRU EMERGENCY PROC: SMOKE DISSIPATED, UNEVENTFULL LANDING. DURINGSDR CA020227007Wire · shorted(CAN) DURING CRUISE FLT, CREW NOTICED FAINT SMOKE SMELL, & NOTICED THAT PROP AUTOFEATHER CIRCUIT BREAKER HAD POPPED. THEY DECIDED TO RETURN TO YYC. DURING APPROACH / LDG PHASE OF FLT, SMELL OF SMOKE BECAME MORE NOTICEABLE. THE LDG & TAXIING TO GATE WENT UNEVE
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